首页> 外文会议>Congress of the International Council of the Aeronautical Sciences; 20060903-08; Hamburg(DE) >A NEW CONCEPT FOR TESTING FATIGUE AND DAMAGE TOLERANCE AT AEROSPACE STRUCTURE
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A NEW CONCEPT FOR TESTING FATIGUE AND DAMAGE TOLERANCE AT AEROSPACE STRUCTURE

机译:在航空结构上测试疲劳和损伤容限的新概念

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Within the 728 Jet Full Scale Fatigue Test, the Spoilers will be tested simultaneously to the wing loading. The spoilers are made of a CFRP sandwich with a solid Honeycomb core. The load assumptions are based on a rectangular pressure distribution on the spoiler surfaces. The loading point of the total spoiler force is the geometry of the trapezoid formed spoilers. The spoiler loads will be introduced in the structure by a pair of bellows on the spoiler surface.
机译:在728 Jet满量程疲劳测试中,扰流板将在机翼载荷的同时进行测试。扰流板由具有坚固蜂窝状芯的CFRP三明治制成。载荷假设基于扰流器表面上的矩形压力分布。总扰流器力的加载点是梯形扰流器的几何形状。扰流板载荷将通过扰流板表面上的一对波纹管引入结构中。

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